AU2006252314B2 - Synthetic resin container having improved shape stability - Google Patents

Synthetic resin container having improved shape stability Download PDF

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Publication number
AU2006252314B2
AU2006252314B2 AU2006252314A AU2006252314A AU2006252314B2 AU 2006252314 B2 AU2006252314 B2 AU 2006252314B2 AU 2006252314 A AU2006252314 A AU 2006252314A AU 2006252314 A AU2006252314 A AU 2006252314A AU 2006252314 B2 AU2006252314 B2 AU 2006252314B2
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AU
Australia
Prior art keywords
container
synthetic resin
main body
resin container
body portion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
AU2006252314A
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AU2006252314A1 (en
Inventor
Hiromichi Saito
Shoji Tanabe
Naoki Tsutsui
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Yoshino Kogyosho Co Ltd
Original Assignee
Yoshino Kogyosho Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from JP2001295405A external-priority patent/JP2003104347A/en
Priority claimed from JP2001295930A external-priority patent/JP4393731B2/en
Priority claimed from JP2001297405A external-priority patent/JP4397554B2/en
Application filed by Yoshino Kogyosho Co Ltd filed Critical Yoshino Kogyosho Co Ltd
Publication of AU2006252314A1 publication Critical patent/AU2006252314A1/en
Application granted granted Critical
Publication of AU2006252314B2 publication Critical patent/AU2006252314B2/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D1/00Containers having bodies formed in one piece, e.g. by casting metallic material, by moulding plastics, by blowing vitreous material, by throwing ceramic material, by moulding pulped fibrous material, by deep-drawing operations performed on sheet material
    • B65D1/02Bottles or similar containers with necks or like restricted apertures, designed for pouring contents
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D1/00Containers having bodies formed in one piece, e.g. by casting metallic material, by moulding plastics, by blowing vitreous material, by throwing ceramic material, by moulding pulped fibrous material, by deep-drawing operations performed on sheet material
    • B65D1/02Bottles or similar containers with necks or like restricted apertures, designed for pouring contents
    • B65D1/0223Bottles or similar containers with necks or like restricted apertures, designed for pouring contents characterised by shape
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D79/00Kinds or details of packages, not otherwise provided for
    • B65D79/005Packages having deformable parts for indicating or neutralizing internal pressure-variations by other means than venting
    • B65D79/008Packages having deformable parts for indicating or neutralizing internal pressure-variations by other means than venting the deformable part being located in a rigid or semi-rigid container, e.g. in bottles or jars
    • B65D79/0084Packages having deformable parts for indicating or neutralizing internal pressure-variations by other means than venting the deformable part being located in a rigid or semi-rigid container, e.g. in bottles or jars in the sidewall or shoulder part thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D1/00Containers having bodies formed in one piece, e.g. by casting metallic material, by moulding plastics, by blowing vitreous material, by throwing ceramic material, by moulding pulped fibrous material, by deep-drawing operations performed on sheet material
    • B65D1/40Details of walls
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D1/00Containers having bodies formed in one piece, e.g. by casting metallic material, by moulding plastics, by blowing vitreous material, by throwing ceramic material, by moulding pulped fibrous material, by deep-drawing operations performed on sheet material
    • B65D1/40Details of walls
    • B65D1/42Reinforcing or strengthening parts or members
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D2501/00Containers having bodies formed in one piece
    • B65D2501/0009Bottles or similar containers with necks or like restricted apertures designed for pouring contents
    • B65D2501/0018Ribs
    • B65D2501/0027Hollow longitudinal ribs
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D2501/00Containers having bodies formed in one piece
    • B65D2501/0009Bottles or similar containers with necks or like restricted apertures designed for pouring contents
    • B65D2501/0018Ribs
    • B65D2501/0036Hollow circonferential ribs
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D2501/00Containers having bodies formed in one piece
    • B65D2501/0009Bottles or similar containers with necks or like restricted apertures designed for pouring contents
    • B65D2501/0081Bottles of non-circular cross-section

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Ceramic Engineering (AREA)
  • Containers Having Bodies Formed In One Piece (AREA)
  • Rigid Containers With Two Or More Constituent Elements (AREA)

Description

AUSTRALIA Patents Act COMPLETE SPECIFICATION (ORIGINAL) Class Int. Class Application Number: Lodged: Complete Specification Lodged: Accepted: Published: Priority Related Art: Name of Applicant: Yoshino Kogyosho Co., Ltd. Actual Inventor(s): Hiromichi Saito, Shoji Tanabe, Naoki Tsutsui Address for Service and Correspondence: PHILLIPS ORMONDE & FITZPATRICK Patent and Trade Mark Attorneys 367 Collins Street Melbourne 3000 AUSTRALIA Invention Title: SYNTHETIC RESIN CONTAINER HAVING IMPROVED SHAPE STABILITY Our Ref: 788331 POF Code: 146127/213247 The following statement is a full description of this invention, including the best method of performing it known to applicant(s): -1- -2 SYNTHETIC RESIN CONTAINER HAVING IMPROVED SHAPE STABILITY The present application is a divisional application from Australian patent 5 application No. 2002332323, the entire disclosure of which is incorporated herein by reference. Technical Field The present invention relates to a thin-walled synthetic resin container, and intends to provide a thin-walled synthetic resin container capable of effectively avoiding 10 lowering of the rigidity of the container, which tends to be caused by its thin-walled nature, to thereby exhibit a required shape stability of the container. Related Art Synthetic resin containers, such as PET bottles made of polyethylene terephthalate resin, have been widely used as containers, e.g., for filling therein foods, 15 beverages, cosmetics or medicines since such containers are light in weight and can thus be easily handled, have transparency to exhibit a refined appearance comparable to glass containers, and can be produced at low cost. This type of synthetic resin container has a relatively low mechanical strength against external forces. Therefore, when the container is gripped at its main body 20 portion for pouring the content out of the container, the container inevitably undergoes deformation at its gripped portion. It is thus a typical countermeasure to appropriately control the container wall thickness and form reinforcing means, e.g., longitudinal ribs, lateral ribs or waists (i.e., circumferential grooves surrounding the main body portion), for improving the resistances of the container to external forces, such as buckling 25 strength and rigidity. Furthermore, there is an increasing demand for thin-walled (or light-weighted) containers so as to reduce the resin amount to be used per one container from a standpoint of effective utilization of resources and reduction in the amount of wastes, resulting in a situation where the rigidity of the container is inevitably further lowered 30 to deal with such a demand. In this instance, particularly in the case of a container having a polygonal cross-section and formed with a waist, the container tends to be deformed in its cross-section into rhombic shape due to the thin-walled nature of the entire container, when external force is applied to the waist portion in a diagonal direction at the corner of the waist position. From such a viewpoint, in connection with -3 a waist-formed synthetic resin container, there is a strong demand for a container structure having higher buckling strength and rigidity, and capable of minimizing deformation in terms of its outer shape of the container even when it is made thin walled. 5 Meanwhile, synthetic resin containers have a relatively low thermal strength, and particularly, containers made of PET resin (polyethylene terephthalate resin) have a limitation on the filling temperature of contents, which must be not higher than approximately 85 to 87*C. Thus, when the contents at temperatures exceeding such a temperature range is filled into the containers, the containers are inevitably deformed 10 due to heat shrinkage thereof. In this respect, there is known a technology as disclosed in JP 7-67732 B2, for example, for improving the heat resistance of containers by carrying out at least two times of biaxial-stretching blow molding before and after an intermediate heat treatment step, and there is indeed a tendency to raise the allowable filling temperatures of contents. 15 However, when this type of targeted container is thin-walled (or light-weighted) so as to reduce the used resin amount (for example, when the used resin amount is reduced from approximately 69 grams to 55 grams or less, in the case of a 2-litre container), the lower region of the container main body portion tends to bulge outwardly due to the self-weight (i.e., hydraulic head) of the contents and due to the 20 affection of heat of the contents, thereby making it difficult to retain the initial shape of the container. Such bulging is particularly marked in containers having pressure reduction absorbing panels, which serve to compensate for the shape deformation of the container due to pressure reduction within the container. Although it is effective to form lateral ribs on a container main body portion so 25 as to retain the outer shape of the container, the ribs may warp due to affection of heat because the container is thin-walled, thereby failing to effectively exhibit the reinforcing function of the ribs. From such a viewpoint, in connection with a synthetic resin container having an improved heat resistance allowing a hot filling of the contents at a relatively high temperature, there is a strong demand for a container structure having an 30 excellent shape stability capable of retaining the initial shape of the container regardless of its thin-walled structure. The discussion of the background to the invention herein is included to explain the context of the invention. This is not to be taken as an admission that any of the 4 material referred to was published, known or part of the common general knowledge in Australia as at the priority date of any of the claims. DISCLOSURE OF THE INVENTION It is therefore a preferred object of the present invention to provide a synthetic resin 5 container capable of addressing at least some of the above-mentioned problems of the prior art. According to a first aspect of the present invention, there is provided a synthetic resin container obtained by biaxial-stretching blow molding, comprising a main body portion provided with a plurality of ridges converging toward associated central convergent points, 10 respectively, such that said ridges form multi-faceted concave walls inclined toward the associated convergent points, respectively, the main body portion provided with a plurality of longitudinal ribs wherein each of said central convergent points has a lateral groove oriented perpendicularly to a main axis of said container. Preferably, the multi-faceted concave walls define the pressure-reduction absorbing 15 panels. Each of the pressure-reduction absorbing panels may exhibit a quadrilateral shape, and the associated ribs of the quadrilateral shape may start from four corners of the quadrilateral shape to converge at the associated central convergent point. BRIEF DESCRIPTION OF THE DRAWINGS The present invention will be described in further detail hereinafter, with reference to 20 the preferred embodiments shown in the drawings FIG. I is a front view of a waist-formed synthetic resin container according to a first embodiment of the present invention. FIG. 2(a) and FIG. 2(b) are a plan view and a bottom view, respectively, of the container of FIG. 1, and FIGS. 2(c) through (i) are cross-sectional views taken along line c-c 25 through line i-i of FIG. 1, respectively. FIG. 3 is a front view of the reinforcing rib of the container of FIG. 1. FIG. 4 is an enlarged view of the essential portion of the container shown in FIG. 1. FIG. 5 is a front view of a synthetic resin container. FIG. 6 is a cross-sectional view taken along line 6-6 of FIG. 5. 30 FIG. 7 is a front view of a synthetic resin container.
-5 FIG. 8 is a front view of a synthetic resin container according to a second embodiment of the present invention. FIG. 9 is a cross-sectional view taken along line 9-9 of FIG. 8. FIG. 10 is a view showing a portion of the pressure-reduction absorbing panel. 5 FIG. 11 is a front view of a synthetic resin container according to a third embodiment of the present invention. FIG. 12 is a cross-sectional view taken along line 12-12 of FIG. 11. FIG. 13 is an enlarged view of the pressure-reduction absorbing panel in the container of FIG. 11. 10 BEST MODE FOR CARRYING OUT THE INVENTION FIG. I through FIG. 4 show a synthetic resin container according to a first embodiment of the present invention. This container has a filling volume of 2.0 litres and is formed in a substantially quadrilateral cross-sectional shape. Reference numeral 11 denotes a waist which divides a main body portion of the container into upper and 15 lower parts. This waist 11 comprises an annular groove I1 a surrounding the main body portion in a manner to become convex toward the interior of the container. Reference numerals 12 denotes reinforcing ribs, respectively, each having a level higher than a groove bottom of the annular groove 1 a and lower than the surface of the main body portion. Each reinforcing rib is formed into an arcuate shape at its 20 outer periphery. These reinforcing ribs 12 are provided at four corners of the main body portion of the container in the present embodiment respectively. Although the waist formed by simply recessing the container main body portion and thereby dividing the main body portion into upper and lower parts is provided for the purpose of improving the rigidity of the container, the thin-walled container has a 25 reduced strength at that region and thus tends to buckle when applied with a load from the upper or bottom portion of the container, besides that the thin-walled container is easily depressed when gripped at the waist portion. FIG. 3 is a front view of the reinforcing rib 12 shown in FIG. 1. When such a reinforcing rib 12 is provided at the waist 11, the reinforcing rib 12 functions as a frame 30 of the container, thereby resulting in an extremely restricted deformation of the container main body portion upon gripping the same, and also resulting in a remarkably improved buckling strength of the container.
-6 Each reinforcing rib 12 is preferably formed into a single arc, so as to avoid stress concentrations and stabilize the outer shape of the container. As can be appreciated from FIG. 4 showing the essential portion of the outer periphery of the reinforcing rib 12 in enlarged scale, the reinforcing rib 12 has a level L 2 lower than the 5 surface level L of the container main body portion and higher than the groove bottom level L, of the annular groove 11 a, so as to effectively exhibit the function of the reinforcing rib 12. Furthermore, the width of the reinforcing rib 12 in the circumferential direction (i.e., around the main body portion) is such that each end portion of the rib extends beyond the associated corner portion of the container and 10 reaches the waist portion positioned at the walled surface of the container. Although the above embodiment has been described in connection with a structure wherein the reinforcing ribs 2 are provided for the container having a quadrilateral cross-sectional shape the present invention is not limited to the illustrated cross-sectional shape. Namely, the present invention is also applicable to containers 15 having a polygonal cross-section, such as rectangular, pentagonal or hexagonal cross section, as well as to containers having a circular cross-section. The present invention is also applicable to containers having a filling volume of not more than 500 milliliters, 1.0 liter, 1.5 liter and even to large-sized containers having a filling volume exceeding 2.0 liters, in addition to the illustrated container of 2.0 liter. There is no particular 20 limitation in terms of the filling volume. It is possible to use a thermoplastic resin such as a polyethylene terephthalate resin as the resin material for the container, and to produce the container by blow molding a preform obtained by extrusion molding or injection molding of such a resin. The container produced by blow molding can be used for either normal 25 temperature filling or high temperature filling of the contents. Particularly, in the case of containers to be filled with a high temperature liquid as the contents, it is possible to utilize a normal molding method for completing the container by performing one time of biaxial-stretching blow molding, and another molding method for completing the container having an improved heat resistance by performing at least twice of biaxial 30 stretching blow molding before and after an intermediate heat treatment step. Then, any of such containers are allowed to have an improved strength by providing reinforcing ribs 12 at the waist, if such waist is provided at the container main body portion.
-7 According to the embodiment described above with reference to FIG. I through FIG. 4, the waist 11 is constituted of the annular groove 1 Ia surrounding the container main body portion so as to be convex toward the interior of the container, and the reinforcing ribs 12 are provided such that each reinforcing rib 12 has a level higher than 5 the groove bottom of the annular groove 11 a and lower than the surface of the main body portion and each reinforcing rib is formed into an arcuate shape at its outer periphery. It is therefore possible to minimize the deformation of the container upon gripping the waist portion, and to remarkably improve the buckling strength and rigidity of the container even when the container is thin-walled. 10 Reference numerals 34 through 39 denote pressure-reduction absorbing panels, respectively, shown as being linearly arranged on the main body portion of the container body 31 by way of example. Panels 36, 37 are shown as having flat surfaces. However, each of the remaining panels 34, 35, 38, 39 are provided with ridges R (inwardly convexed ridges) 15 converging at a central convergent point Ro of the applicable panel so that the ridges R define a multi-faceted concave wall comprising wall surfaces 34a through 34d, 35a through 35d, 38a through 38d or 39a through 39d, which are inclined toward the associated convergent point Ro. For clarity of illustration, reference numerals to these surfaces are not shown in FIG. 1 but can be seen in FIG. 8. The details of panels 34, 35, 20 38, 39 are shown in FIG. 10. FIG.5 and FIG. 6 show a synthetic resin container. Reference numeral 21 denotes a container body, and reference numeral 22 denotes a mouth portion integral with the container body 21. Furthermore, reference numeral 23 denotes a groove portion for dividing the container body 21 into upper and lower parts to thereby enhance 25 the rigidity of the container, and reference numerals 24 denotes pressure-reduction absorbing panels, respectively. Each pressure-reduction absorbing panel 24 has a function for preventing a shape deformation of the container due to a volume change thereof as a result of cooling of the contents therein. Reference numeral 25 denotes reinforcing lateral ribs formed at the main body 30 portion of the container so as to extend across the pressure-reduction absorbing panels 24, respectively. Each lateral rib 25 has a concave portion 25a at a central region (i.e., the central region in the longitudinal direction) of the lateral rib itself, such that the concave portion is positioned at the same level as the surface of the container main body -8 portion, or the concave portion forms a slight step relative to the surface of the container main body portion. Reference numerals 26 denotes reinforcing longitudinal ribs alternately arranged between the lateral ribs 25, respectively, and reference numerals 27 denotes pillars 5 formed at four locations around the main body portion. Each pillar 27 has a longitudinally elongated concave surface 27a formed into a polygonal line shape and extended along a main axis P of the container. There is known a synthetic resin container formed by one time of biaxial stretching blow molding, or another synthetic resin container formed by at least two 10 times of biaxial-stretching blow molding before and after an intermediate heat treatment step, such as that disclosed in JP-7-67732 B2. In this type of container, the residual stress in the container main body portion is remarkably mitigated and the strength against external heat is enhanced by virtue of the increased density of the resin. However, even if lateral ribs are provided to ensure the shape stability of this type of 15 container when the container is thin-walled to reduce the resin amount to be used per one container, the lateral ribs inevitably tend to warp due to the self-weight (hydraulic head) of the contents themselves and due to the affection of the heat possessed by the contents. In such instance, the lateral ribs do not restore due to the plastic deformation of the lateral ribs themselves even after cooling of the contents, thereby resulting in a 20 poor appearance of the container. According to the container of FIG. 5 and FIG. 6, however, each concave portion 25a provided at the associated lateral rib 25 is positioned at the same level as the surface of the container or forms a slight step relative to the surface of the container, so as to prevent warpage of the lateral rib 25 as a whole and thereby retain the initial shape of the container. Further, the lateral rib 25 effectively 25 exhibited the intended function to keep the container in a highly rigid state. It is preferred for the lateral ribs 25 to be arranged along the widthwise direction of the pressure-reduction absorbing panels 24, respectively, so as to extend across these panels. Although each lateral rib 25 has been exemplarily shown in FIG. 5 to have such 30 a length that the opposite ends of the lateral rib reach the associated pillars 27, respectively, the length of the lateral rib may be preferably short of the pillars 27 so as not to affect the function of the pillars 27. Further, each pillar 27 is preferably constituted to have the concave surface 27a formed into the polygonal line shape or a -9 convex surface 27a in an R shape, such that the pillar 27 does not easily buckle even upon application of a load from the upper or lower portion of the container. The longitudinal ribs 26 may be arranged between the lateral ribs 25 and adjacent to the pillars 27, respectively. Provision of such longitudinal ribs 26 ensures 5 that, even when the container is to be deformed due to a load upon gripping the container, the deformation of the container always occurs at constant locations i.e., in the directions of the end portions of lateral ribs 25, in the present embodiment, so that the container is immediately restored to its initial shape upon releasing of the load that caused the deformation. This means that it is possible to improve the restoring 10 performance of the container after deformation. FIG. 7 shows a synthetic resin container wherein the region around each longitudinal rib 26 is formed as a concave portion 28. The concave portion 28 is lower than the surface of the container main body portion such that the contour shape of the longitudinal rib 26 is embossed upon molding the container to thereby further enhance 15 the reinforcing effect near the corner portion of the container, while each lateral rib 24 is made to have a reduced length such that the opposite ends thereof are short of the associated pillars 27, respectively. Such a constitution ensures that the buckling strength is further enhanced in the container having a quadrilateral cross-section, and the restoring ability of the container after deformation is further improved. 20 When containers are produced by adopting a polyethylene terephthalate resin as the resin for the container and conducting two times of biaxial-stretching blow molding before and after an intermediate of heat treatment step, the following procedure shall be followed. First of all, a preform obtained by extrusion molding or injection molding is 25 heated to a temperature which allows exhibition of stretching effect, e.g., to a temperature range of 70 to 130"C, and more preferably 90 to 120'C. Then, the first time of biaxial-stretching blow molding is conducted under a temperature condition of 50 to 230"C, more preferably 70 to 180"C, with a surface stretching ratio of 4 to 22 (more preferably 6 to 15, into an oversized intermediate body having a volume which is 30 about 1.2 to 2.5 times that of the finished container). Next, the thus obtained blow molded body is applied with a forced heat treatment at a temperature in a range of 1 10 to 255 0 C, more preferably 130 to 200"C, so as to be shrunk to a size which is about 0.60 to 0.95 times that of the finished container, to thereby remove the residual stress in the - 10 article. Subsequently, there is conducted a second time of biaxial-stretching blow molding at a temperature in a range of 60 to 170*C, more preferably 80 to 150 0 C. It is noted that the container according to the present invention may be of course molded by one time of biaxial-stretching blow molding, without following the above conditions. 5 In this way, according to the container shown in FIG. 5 and FIG. 6 or the container shown in FIG. 7, the resin container having an improved heat resistance is provided with the reinforcing lateral ribs 27 having the concave portions 27a, respectively, each of which is positioned at the same level as the surface of the container or forms a slight step relative to the surface of the container, thereby making it possible 10 to maintain an improved shape stability even when the container is thin-walled for reducing the used amount of resin. FIG. 8 through FIG. 10 show a synthetic resin container according to a second embodiment of the present invention. Reference numeral 31 denotes a container body, reference numerals 32 denotes reinforcing lateral ribs, respectively, appropriately 15 formed at the main body portion of the container body 31, reference numerals 33 denotes reinforcing longitudinal ribs, respectively, appropriately formed at the main body portion of the container body 31, and reference numerals 34 through 39 denote pressure-reduction absorbing panels, respectively, shown as being linearly arranged on the main body portion of the container body 31 by way of example. 20 While the panels 36, 37 among the pressure-reduction absorbing panels 34 through 39 are shown as having flat surfaces, respectively, each of the remaining panels 34, 35, 38, 39 is provided with ridges R (inwardly convexed ridges) converging at a central convergent point Ro of the applicable panel so that the ridges R define a multi faceted concave wall comprising wall surfaces 34a through 34d, 35a, through 35d, 38a 25 through 38d or 39a through 39d, which are inclined toward the associated convergent point Ro. The details of the panels 34, 35, 38, 39 are shown in FIG. 10. By forming the pressure-reduction absorbing panels 34, 35, 38, 39 into the multi-faceted concave walls according to the embodiments of FIG. I through FIG. 4 and FIG. 8 through FIG. 10, respectively, it is possible for the ridges R to act as reinforcing 30 frames of the panels, respectively, thereby advantageously avoiding bulging of the container due to the hydraulic head of the contents. Further, since the shape deformation of the container due to the pressure reduction is compensated for by the -11 entirety of each pressure-reduction absorbing panels 34, 35, 38, 39, this function is not affected by the associated ridges R. Although the pressure-reduction absorbing panels 36, 37 are embodied to have flat surfaces in the embodiment of FIG. 8, such an arrangement is to stabilize the shape 5 of the container, and it is possible in the present invention to constitute the container by appropriately combining panels having flat surfaces, with panels having multi-faceted concave walls. FIG 11. through FIG. 13 show a synthetic resin container according to a third embodiment of the present invention. This embodiment is achieved when the 10 convergent point Ro of each of the pressure-reduction absorbing panels 34, 35, 38, 39 in the embodiment of FIG. 8 through FIG. 10 is provided with a lateral groove 40 oriented perpendicularly to the main axis P of the container. The provision of such lateral grooves 40 allows a further suppression of bulging of the pressure-reduction absorbing panels 34, 35, 38, 39 due to the hydraulic head of the contents. 15 Although the embodiment shown in FIG. 11 through FIG. 13 has been described with reference to an arrangement wherein the multi-faceted concave walls are applied to the pressure-reduction absorbing panels 34, 35, 38, 39 having a reduced wall thickness, such multi-faceted concave walls can be directly provided at the main body portion of the container body 31, without being limited to the application to the pressure-reduction 20 absorbing panels only. According to the embodiment of FIG. 11 through FIG. 13, the main body portion of the synthetic resin container is provided with multiple ridges R converging toward the associated central convergent points Ro, respectively, such that the ridges R define multi-faceted concave walls that are inclined toward the associated convergent 25 points Ro, respectively. Therefore, it is possible to retain a high shape stability of a resin container having an excellent heat resistance, even when the container is thin walled to reduce the used amount of resin. It will be appreciated from the foregoing description that, according to the present invention, it is possible to solve various problems of the prior art and realize a 30 thin-walled synthetic resin container capable of effectively avoiding lowering of the rigidity of the container due to its thin-walled nature, to thereby exhibit a required shape stability of the container.
- 12 It is needless to say that the present invention is not limited to the above mentioned embodiments, and may be carried out with numerous variants.

Claims (4)

1. A synthetic resin container obtained by biaxial-stretching blow molding, comprising: 5 a main body portion provided with a plurality of ridges converging toward associated central convergent points, respectively, such that said ridges form multi-faceted concave walls inclined toward the associated convergent points, respectively, the main body portion provided with a plurality of longitudinal ribs wherein each of said central convergent points has a lateral groove oriented perpendicularly to a main axis of said container. 10
2. A synthetic resin container according to claim 1, wherein said multi-faceted concave walls define a pressure-reduction absorbing panel.
3. A synthetic resin container according to claim 2, wherein said pressure-reduction 15 absorbing panel exhibits a quadrilateral shape, and the associated ridges of said quadrilateral shape start from four corners of said quadrilateral shape to converge at the associated central convergent point.
4. A synthetic resin container substantially as hereinbefore described with reference to the 20 accompany drawings.
AU2006252314A 2001-09-27 2006-12-28 Synthetic resin container having improved shape stability Ceased AU2006252314B2 (en)

Applications Claiming Priority (8)

Application Number Priority Date Filing Date Title
JP2001295405A JP2003104347A (en) 2001-09-27 2001-09-27 Waisted container made of synthetic resin
JP2001-297405 2001-09-27
JP2001295930A JP4393731B2 (en) 2001-09-27 2001-09-27 Synthetic resin container with excellent shape retention
JP2001-295930 2001-09-27
JP2001-295405 2001-09-27
JP2001297405A JP4397554B2 (en) 2001-09-27 2001-09-27 Synthetic resin container with excellent shape retention
AU2002332323A AU2002332323B2 (en) 2001-09-27 2002-09-26 Synthetic resin container with shape retainability
PCT/JP2002/009976 WO2003029087A1 (en) 2001-09-27 2002-09-26 Synthetic resin container with shape retainability

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AU2006252314B2 true AU2006252314B2 (en) 2010-04-22

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EP (3) EP1431192B1 (en)
KR (2) KR100706850B1 (en)
CN (1) CN1260099C (en)
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DE (3) DE60228980D1 (en)
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DE60226081D1 (en) 2008-05-21
CN1558855A (en) 2004-12-29
EP1561692A3 (en) 2006-08-02
AU2006252313A1 (en) 2007-01-25
KR100706850B1 (en) 2007-04-13
DE60228980D1 (en) 2008-10-30
KR20060110009A (en) 2006-10-23
EP1561692A2 (en) 2005-08-10
AU2006252314A1 (en) 2007-01-25
AU2006252313B2 (en) 2010-05-27
EP1574439A3 (en) 2006-08-02
DE60225730T2 (en) 2009-04-23
DE60226081T2 (en) 2009-06-25
EP1561692B1 (en) 2008-03-19
EP1431192A1 (en) 2004-06-23
WO2003029087A1 (en) 2003-04-10
EP1431192A4 (en) 2005-03-02
EP1574439A2 (en) 2005-09-14
EP1574439B1 (en) 2008-04-09
TWI232192B (en) 2005-05-11
US7552833B2 (en) 2009-06-30
EP1431192B1 (en) 2008-09-17
AU2002332323B2 (en) 2007-01-04
US20050045645A1 (en) 2005-03-03
CN1260099C (en) 2006-06-21
KR20040033072A (en) 2004-04-17
KR100730334B1 (en) 2007-06-19
DE60225730D1 (en) 2008-04-30

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